View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 52678U 26145.41656609 +.00000000 +00000-0 +26131-5 0 00004
2 52678 53.2108 159.7830 0001077 64.5416 295.5688 15.08837714 00
| Epoch (UTC): | 25 May 2026 09:59:51 |
| Eccentricity: | 0.0001077 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 159.7830° |
| argument of perigee: | 64.5416° |
| revolutions per day: | 15.08837714 |
| mean anomaly at epoch: | 295.5688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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